View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48796U 26145.56937447 +.00000000 +00000-0 +22292-3 0 00000
2 48796 87.8990 263.7035 0001401 81.7776 278.3513 13.15549796 04
| Epoch (UTC): | 25 May 2026 13:39:53 |
| Eccentricity: | 0.0001401 |
| inclination: | 87.8990° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7035° |
| argument of perigee: | 81.7776° |
| revolutions per day: | 13.15549796 |
| mean anomaly at epoch: | 278.3513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|