View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00005U 26087.99216418 +.00000000 +00000-0 +23343-3 0 00009
2 00005 34.2408 201.8051 1836428 136.8846 239.1174 10.85962456 06
| Epoch (UTC): | 28 March 2026 23:48:42 |
| Eccentricity: | 0.1836428 |
| inclination: | 34.2408° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 201.8051° |
| argument of perigee: | 136.8846° |
| revolutions per day: | 10.85962456 |
| mean anomaly at epoch: | 239.1174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|