View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08846U 26040.24809487 +.00000000 +00000-0 +12996-3 0 00003
2 08846 81.2231 117.0806 0036737 95.7358 264.8003 14.08991718 02
| Epoch (UTC): | 09 February 2026 05:57:15 |
| Eccentricity: | 0.0036737 |
| inclination: | 81.2231° |
| perigee height: | 836 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 117.0806° |
| argument of perigee: | 95.7358° |
| revolutions per day: | 14.08991718 |
| mean anomaly at epoch: | 264.8003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|