View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08800U 26067.09179117 +.00000000 +00000-0 +63992-4 0 00008
2 08800 81.2540 357.0629 0093942 162.5235 197.9208 14.10650331 01
| Epoch (UTC): | 08 March 2026 02:12:10 |
| Eccentricity: | 0.0093942 |
| inclination: | 81.2540° |
| perigee height: | 789 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 357.0629° |
| argument of perigee: | 162.5235° |
| revolutions per day: | 14.10650331 |
| mean anomaly at epoch: | 197.9208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|