View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52707U 26145.41946073 +.00000000 +00000-0 +99123-3 0 00003
2 52707 53.2146 149.4178 0002309 48.5577 311.5613 15.09838510 08
| Epoch (UTC): | 25 May 2026 10:04:01 |
| Eccentricity: | 0.0002309 |
| inclination: | 53.2146° |
| perigee height: | 535 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 149.4178° |
| argument of perigee: | 48.5577° |
| revolutions per day: | 15.09838510 |
| mean anomaly at epoch: | 311.5613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|