View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54114U 26145.41481832 +.00000000 +00000-0 +19977-3 0 00003
2 54114 87.9150 309.5085 0001578 94.7558 265.3755 13.19726207 07
| Epoch (UTC): | 25 May 2026 09:57:20 |
| Eccentricity: | 0.0001578 |
| inclination: | 87.9150° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5085° |
| argument of perigee: | 94.7558° |
| revolutions per day: | 13.19726207 |
| mean anomaly at epoch: | 265.3755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|