View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 44624U 26145.58277509 +.00000000 +00000-0 +00000-0 0 00004
2 44624 0.0654 341.0399 0003168 79.7765 27.1427 1.00271610 06
| Epoch (UTC): | 25 May 2026 13:59:11 |
| Eccentricity: | 0.0003168 |
| inclination: | 0.0654° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 341.0399° |
| argument of perigee: | 79.7765° |
| revolutions per day: | 1.00271610 |
| mean anomaly at epoch: | 27.1427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|