View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54123U 26145.38007470 +.00000000 +00000-0 +10164-3 0 00000
2 54123 87.9160 309.5118 0001662 78.9083 281.2236 13.19725387 05
| Epoch (UTC): | 25 May 2026 09:07:18 |
| Eccentricity: | 0.0001662 |
| inclination: | 87.9160° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5118° |
| argument of perigee: | 78.9083° |
| revolutions per day: | 13.19725387 |
| mean anomaly at epoch: | 281.2236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|