View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62820U 26145.44333531 +.00000000 +00000-0 +59925-3 0 00008
2 62820 53.1610 312.8046 0001682 90.4918 269.6276 15.31722609 02
| Epoch (UTC): | 25 May 2026 10:38:24 |
| Eccentricity: | 0.0001682 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 312.8046° |
| argument of perigee: | 90.4918° |
| revolutions per day: | 15.31722609 |
| mean anomaly at epoch: | 269.6276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|