View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54004U 26145.50574777 +.00000000 +00000-0 -68422-4 0 00003
2 54004 53.2139 228.9609 0001404 82.2324 277.8828 15.08844405 05
| Epoch (UTC): | 25 May 2026 12:08:16 |
| Eccentricity: | 0.0001404 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 228.9609° |
| argument of perigee: | 82.2324° |
| revolutions per day: | 15.08844405 |
| mean anomaly at epoch: | 277.8828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|