View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51874U 26145.38297854 +.00000000 +00000-0 +91546-4 0 00001
2 51874 53.2135 24.8277 0001434 93.0074 267.1082 15.08836824 02
| Epoch (UTC): | 25 May 2026 09:11:29 |
| Eccentricity: | 0.0001434 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 24.8277° |
| argument of perigee: | 93.0074° |
| revolutions per day: | 15.08836824 |
| mean anomaly at epoch: | 267.1082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|