View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58969U 26144.90631953 +.00000000 +00000-0 +21672-2 0 00003
2 58969 53.1603 299.7451 0001659 83.0103 277.1088 15.34275995 03
| Epoch (UTC): | 24 May 2026 21:45:06 |
| Eccentricity: | 0.0001659 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 299.7451° |
| argument of perigee: | 83.0103° |
| revolutions per day: | 15.34275995 |
| mean anomaly at epoch: | 277.1088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|