View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48801U 26145.37289775 +.00000000 +00000-0 +19136-3 0 00003
2 48801 87.8996 263.7400 0001956 99.1366 260.9986 13.15547457 09
| Epoch (UTC): | 25 May 2026 08:56:58 |
| Eccentricity: | 0.0001956 |
| inclination: | 87.8996° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7400° |
| argument of perigee: | 99.1366° |
| revolutions per day: | 13.15547457 |
| mean anomaly at epoch: | 260.9986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|