View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60390U 26145.64858022 +.00000000 +00000-0 +12099-3 0 00008
2 60390 88.9698 282.2759 0015178 94.0253 266.2633 13.51008357 09
| Epoch (UTC): | 25 May 2026 15:33:57 |
| Eccentricity: | 0.0015178 |
| inclination: | 88.9698° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 282.2759° |
| argument of perigee: | 94.0253° |
| revolutions per day: | 13.51008357 |
| mean anomaly at epoch: | 266.2633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|