View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54084U 26145.60517088 +.00000000 +00000-0 +93232-4 0 00000
2 54084 53.2105 348.9776 0002532 94.4081 265.7201 15.08831120 03
| Epoch (UTC): | 25 May 2026 14:31:26 |
| Eccentricity: | 0.0002532 |
| inclination: | 53.2105° |
| perigee height: | 538 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 348.9776° |
| argument of perigee: | 94.4081° |
| revolutions per day: | 15.08831120 |
| mean anomaly at epoch: | 265.7201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|