View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52320U 26145.64249999 +.00000000 +00000-0 +21270-3 0 00000
2 52320 97.3410 219.1474 0002252 48.8734 311.2693 15.16284302 08
| Epoch (UTC): | 25 May 2026 15:25:11 |
| Eccentricity: | 0.0002252 |
| inclination: | 97.3410° |
| perigee height: | 516 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 219.1474° |
| argument of perigee: | 48.8734° |
| revolutions per day: | 15.16284302 |
| mean anomaly at epoch: | 311.2693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|