View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60578U 26145.21522752 +.00000000 +00000-0 +41628-3 0 00007
2 60578 97.6713 226.2045 0007145 123.1592 237.0322 15.06840349 01
| Epoch (UTC): | 25 May 2026 05:09:55 |
| Eccentricity: | 0.0007145 |
| inclination: | 97.6713° |
| perigee height: | 541 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 226.2045° |
| argument of perigee: | 123.1592° |
| revolutions per day: | 15.06840349 |
| mean anomaly at epoch: | 237.0322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|