View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53191U 26145.42670454 +.00000000 +00000-0 +25507-2 0 00003
2 53191 97.6003 206.2377 0000971 47.4821 312.6497 15.22912115 07
| Epoch (UTC): | 25 May 2026 10:14:27 |
| Eccentricity: | 0.0000971 |
| inclination: | 97.6003° |
| perigee height: | 496 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 206.2377° |
| argument of perigee: | 47.4821° |
| revolutions per day: | 15.22912115 |
| mean anomaly at epoch: | 312.6497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|