View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65182U 26145.14858647 +.00000000 +00000-0 +13257-2 0 00006
2 65182 97.4489 17.6171 0001959 87.1644 272.9808 15.05643285 07
| Epoch (UTC): | 25 May 2026 03:33:57 |
| Eccentricity: | 0.0001959 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6171° |
| argument of perigee: | 87.1644° |
| revolutions per day: | 15.05643285 |
| mean anomaly at epoch: | 272.9808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|