View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08800U 26064.25460669 +.00000000 +00000-0 +45150-4 0 00004
2 08800 81.2539 359.8247 0093852 170.4668 189.8314 14.10649897 06
| Epoch (UTC): | 05 March 2026 06:06:38 |
| Eccentricity: | 0.0093852 |
| inclination: | 81.2539° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 359.8247° |
| argument of perigee: | 170.4668° |
| revolutions per day: | 14.10649897 |
| mean anomaly at epoch: | 189.8314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|