View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62271U 26145.16544066 +.00000000 +00000-0 +17959-2 0 00004
2 62271 42.9989 316.2022 0002894 287.7115 72.3436 15.70929723 01
| Epoch (UTC): | 25 May 2026 03:58:14 |
| Eccentricity: | 0.0002894 |
| inclination: | 42.9989° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 316.2022° |
| argument of perigee: | 287.7115° |
| revolutions per day: | 15.70929723 |
| mean anomaly at epoch: | 72.3436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|