View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65466U 26145.03667038 +.00000000 +00000-0 +76660-3 0 00009
2 65466 53.1599 263.4951 0001915 76.9505 283.1711 15.33597128 06
| Epoch (UTC): | 25 May 2026 00:52:48 |
| Eccentricity: | 0.0001915 |
| inclination: | 53.1599° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 263.4951° |
| argument of perigee: | 76.9505° |
| revolutions per day: | 15.33597128 |
| mean anomaly at epoch: | 283.1711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|