View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58384U 26145.03337727 +.00000000 +00000-0 +42891-4 0 00009
2 58384 53.1612 5.4691 0001050 80.8794 279.2327 15.34394344 07
| Epoch (UTC): | 25 May 2026 00:48:03 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.1612° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 5.4691° |
| argument of perigee: | 80.8794° |
| revolutions per day: | 15.34394344 |
| mean anomaly at epoch: | 279.2327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|