View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24876U 26145.26688860 +.00000000 +00000-0 +00000-0 0 00002
2 24876 55.9835 99.4710 0101328 56.5207 304.4123 2.00563829 06
| Epoch (UTC): | 25 May 2026 06:24:19 |
| Eccentricity: | 0.0101328 |
| inclination: | 55.9835° |
| perigee height: | 19913 km |
| apogee height: | 20451 km |
| right ascension of ascending node: | 99.4710° |
| argument of perigee: | 56.5207° |
| revolutions per day: | 2.00563829 |
| mean anomaly at epoch: | 304.4123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|