View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61536U 26145.38055713 +.00000000 +00000-0 +72253-5 0 00008
2 61536 53.1601 218.1204 0001234 81.4257 278.6901 15.69708406 03
| Epoch (UTC): | 25 May 2026 09:08:00 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 218.1204° |
| argument of perigee: | 81.4257° |
| revolutions per day: | 15.69708406 |
| mean anomaly at epoch: | 278.6901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|