View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53172U 26145.48325250 +.00000000 +00000-0 -15150-3 0 00004
2 53172 53.2146 174.2902 0000818 87.1688 272.9397 15.08823207 06
| Epoch (UTC): | 25 May 2026 11:35:53 |
| Eccentricity: | 0.0000818 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.2902° |
| argument of perigee: | 87.1688° |
| revolutions per day: | 15.08823207 |
| mean anomaly at epoch: | 272.9397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|