View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42801U 26145.08509955 +.00000000 +00000-0 +00000-0 0 00007
2 42801 0.0197 57.9077 0003546 21.4159 195.8856 1.00267545 01
| Epoch (UTC): | 25 May 2026 02:02:32 |
| Eccentricity: | 0.0003546 |
| inclination: | 0.0197° |
| perigee height: | 35773 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 57.9077° |
| argument of perigee: | 21.4159° |
| revolutions per day: | 1.00267545 |
| mean anomaly at epoch: | 195.8856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|