View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59938U 26145.32155397 +.00000000 +00000-0 +12499-3 0 00008
2 59938 43.0034 259.6635 0001533 266.7167 93.3509 15.27585576 03
| Epoch (UTC): | 25 May 2026 07:43:02 |
| Eccentricity: | 0.0001533 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.6635° |
| argument of perigee: | 266.7167° |
| revolutions per day: | 15.27585576 |
| mean anomaly at epoch: | 93.3509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|