# Long March 2D | Yaogan 35 Group 05

**URL:** <https://www.forumastronautico.it/t/long-march-2d-yaogan-35-group-05/45956>\
**Category:** Archivio lanci\
**Tags:** lunga-marcia, lanci-2022, cnsa, lanci-casc, lunga-marcia-2d\
**Created:** [5 Settembre 2022, 3:34pm UTC](https://www.forumastronautico.it/t/long-march-2d-yaogan-35-group-05/45956 "2022-09-05T15:34:11Z")\
**Posts on this page:** 1\
**Showing post:** 1

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**Author:** ![astronautibot](https://www.forumastronautico.it/user_avatar/www.forumastronautico.it/astronautibot/32/97479_2.png) [@astronautibot](https://www.forumastronautico.it/u/astronautibot)\
**Post date:** [5 Settembre 2022, 3:34pm UTC](https://www.forumastronautico.it/t/long-march-2d-yaogan-35-group-05/45956/1 "2022-09-05T15:34:11Z")

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> **Long March 2D | Yaogan 35 Group 05**
>
> **Starts:** 6 Settembre 2022, 4:09am (Etc/UTC)\
> **Ends:** 6 Settembre 2022, 4:29am (Etc/UTC)\
> **Location:** www.openstreetmap.org/#map=17/28.2470590/102.0290080&layers=N

### Informazioni sulla missione

| | |
| --- | --- |
| Lancio | 2022-09-06T04:19:00 |
| Esito | **SUCCESSO** |
| Tipo missione | Governativo/Top Secret |
| Orbita | Orbita bassa terrestre (LEO) |
| Rampa | Launch Complex 3 (LC-3/LA-1), Centro di lancio satelliti dello Xichang, Repubblica Popolare Cinese (CHN) [🗺](http://www.openstreetmap.org/?mlat=28.247059&mlon=102.029008&zoom=20) |

### Lanciatore

| | |
| --- | --- |
| Nome | [Long March 2D](https://www.forumastronautico.it/t/37811) [Wiki](https://en.wikipedia.org/wiki/Long_March_(rocket_family)) |
| Costruttore | China Aerospace Science and Technology Corporation [Wiki](https://en.wikipedia.org/wiki/China_Aerospace_Science_and_Technology_Corporation) [Info](https://english.spacechina.com/) |
| Fornitore servizi di lancio | China Aerospace Science and Technology Corporation [Wiki](https://en.wikipedia.org/wiki/China_Aerospace_Science_and_Technology_Corporation) [Info](https://english.spacechina.com/) |
| Primo volo | 1992-08-09 |
| Numero stadi | 2 |
| Altezza | 38,30 m |
| Diametro | 3,35 m |
| Peso al lancio | 232 t |
| Spinta al decollo | 2.962 kN |
| Capacità di carico | LEO: 3.500 kg  
GTO: 0 kg |
| Successi/Lanci totali | 99/100 (68 consecutivi) |
| Booster | None |

Ultimo aggiornamento: 2026-09-09T20:00:40 con AstronautiBOT 2026.09.07 - Fonte: [LaunchLibrary2 API](https://ll.thespacedevs.com/2.2.0/launch/fdc9abba-84fc-41bf-8e16-8e7a0d31ea1a/?format=json)

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