View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00005U 26046.86993169 +.00000000 +00000-0 +15674-3 0 00003
2 00005 34.2578 328.7290 1838768 311.4405 34.1899 10.85949236 07
| Epoch (UTC): | 15 February 2026 20:52:42 |
| Eccentricity: | 0.1838768 |
| inclination: | 34.2578° |
| perigee height: | 652 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 328.7290° |
| argument of perigee: | 311.4405° |
| revolutions per day: | 10.85949236 |
| mean anomaly at epoch: | 34.1899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|