View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62321U 26145.47755617 +.00000000 +00000-0 +80093-3 0 00000
2 62321 53.1573 184.2419 0000894 95.5161 264.5942 15.30214094 08
| Epoch (UTC): | 25 May 2026 11:27:40 |
| Eccentricity: | 0.0000894 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.2419° |
| argument of perigee: | 95.5161° |
| revolutions per day: | 15.30214094 |
| mean anomaly at epoch: | 264.5942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|