View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53977U 26145.54766198 +.00000000 +00000-0 -48368-4 0 00002
2 53977 53.2113 234.2030 0001243 84.2517 275.8617 15.08842409 06
| Epoch (UTC): | 25 May 2026 13:08:37 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.2030° |
| argument of perigee: | 84.2517° |
| revolutions per day: | 15.08842409 |
| mean anomaly at epoch: | 275.8617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|