View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58986U 26145.14346582 +.00000000 +00000-0 +62856-4 0 00001
2 58986 53.1615 301.9221 0001261 98.7355 261.3788 15.30184948 02
| Epoch (UTC): | 25 May 2026 03:26:35 |
| Eccentricity: | 0.0001261 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 301.9221° |
| argument of perigee: | 98.7355° |
| revolutions per day: | 15.30184948 |
| mean anomaly at epoch: | 261.3788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|