View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65492U 26145.36151832 +.00000000 +00000-0 +96205-3 0 00001
2 65492 53.1582 273.8179 0001192 99.4993 260.6144 15.34416750 04
| Epoch (UTC): | 25 May 2026 08:40:35 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.8179° |
| argument of perigee: | 99.4993° |
| revolutions per day: | 15.34416750 |
| mean anomaly at epoch: | 260.6144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|