View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60127U 26145.41149977 +.00000000 +00000-0 +52917-5 0 00008
2 60127 53.1618 30.2999 0001243 91.2684 268.8460 15.31696779 02
| Epoch (UTC): | 25 May 2026 09:52:33 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1618° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.2999° |
| argument of perigee: | 91.2684° |
| revolutions per day: | 15.31696779 |
| mean anomaly at epoch: | 268.8460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|