View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40034U 26088.18466343 +.00000000 +00000-0 +58850-3 0 00002
2 40034 97.7670 245.2151 0042711 322.6531 37.1719 14.90309138 02
| Epoch (UTC): | 29 March 2026 04:25:54 |
| Eccentricity: | 0.0042711 |
| inclination: | 97.7670° |
| perigee height: | 567 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 245.2151° |
| argument of perigee: | 322.6531° |
| revolutions per day: | 14.90309138 |
| mean anomaly at epoch: | 37.1719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|