View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53676U 26145.38596726 +.00000000 +00000-0 +42160-3 0 00000
2 53676 97.4465 25.3603 0002166 73.2908 286.8557 15.05619519 00
| Epoch (UTC): | 25 May 2026 09:15:47 |
| Eccentricity: | 0.0002166 |
| inclination: | 97.4465° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.3603° |
| argument of perigee: | 73.2908° |
| revolutions per day: | 15.05619519 |
| mean anomaly at epoch: | 286.8557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|