View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61682U 26072.17458190 +.00000000 +00000-0 +26684-4 0 00008
2 61682 53.1602 74.5629 0001313 90.8182 269.2969 15.30192906 00
| Epoch (UTC): | 13 March 2026 04:11:23 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 74.5629° |
| argument of perigee: | 90.8182° |
| revolutions per day: | 15.30192906 |
| mean anomaly at epoch: | 269.2969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|