View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48048U 26145.47986602 +.00000000 +00000-0 +84038-3 0 00003
2 48048 87.8950 324.7328 0001691 99.5294 260.6026 13.13469034 03
| Epoch (UTC): | 25 May 2026 11:31:00 |
| Eccentricity: | 0.0001691 |
| inclination: | 87.8950° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7328° |
| argument of perigee: | 99.5294° |
| revolutions per day: | 13.13469034 |
| mean anomaly at epoch: | 260.6026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|