View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54067U 26145.30612120 +.00000000 +00000-0 +83773-4 0 00000
2 54067 53.2124 359.9496 0001092 101.1838 258.9277 15.08839111 07
| Epoch (UTC): | 25 May 2026 07:20:48 |
| Eccentricity: | 0.0001092 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 359.9496° |
| argument of perigee: | 101.1838° |
| revolutions per day: | 15.08839111 |
| mean anomaly at epoch: | 258.9277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|