View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48863U 26145.62361690 +.00000000 +00000-0 +18387-3 0 00003
2 48863 34.9960 289.0428 0003837 317.7083 42.3329 15.02557923 07
| Epoch (UTC): | 25 May 2026 14:58:00 |
| Eccentricity: | 0.0003837 |
| inclination: | 34.9960° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 289.0428° |
| argument of perigee: | 317.7083° |
| revolutions per day: | 15.02557923 |
| mean anomaly at epoch: | 42.3329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|