View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04952U 26105.91471338 +.00000000 +00000-0 +41045-4 0 00001
2 04952 29.6682 300.8021 0079637 190.2412 328.6204 13.58635496 05
| Epoch (UTC): | 15 April 2026 21:57:11 |
| Eccentricity: | 0.0079637 |
| inclination: | 29.6682° |
| perigee height: | 982 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 300.8021° |
| argument of perigee: | 190.2412° |
| revolutions per day: | 13.58635496 |
| mean anomaly at epoch: | 328.6204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|