View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42915U 26145.58147508 +.00000000 +00000-0 +00000-0 0 00000
2 42915 3.4466 2.1985 0014204 101.7522 337.0821 1.00272147 08
| Epoch (UTC): | 25 May 2026 13:57:19 |
| Eccentricity: | 0.0014204 |
| inclination: | 3.4466° |
| perigee height: | 35727 km |
| apogee height: | 35846 km |
| right ascension of ascending node: | 2.1985° |
| argument of perigee: | 101.7522° |
| revolutions per day: | 1.00272147 |
| mean anomaly at epoch: | 337.0821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|