View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58538U 26145.49555336 +.00000000 +00000-0 -11451-5 0 00008
2 58538 53.1618 65.3546 0001343 87.9546 272.1610 15.34383521 08
| Epoch (UTC): | 25 May 2026 11:53:35 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.3546° |
| argument of perigee: | 87.9546° |
| revolutions per day: | 15.34383521 |
| mean anomaly at epoch: | 272.1610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|