View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62013U 26145.39156738 +.00000000 +00000-0 +16974-2 0 00004
2 62013 53.1582 23.0382 0000476 209.0260 151.0731 15.69775235 00
| Epoch (UTC): | 25 May 2026 09:23:51 |
| Eccentricity: | 0.0000476 |
| inclination: | 53.1582° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 23.0382° |
| argument of perigee: | 209.0260° |
| revolutions per day: | 15.69775235 |
| mean anomaly at epoch: | 151.0731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|