View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15199U 26150.51538596 +.00000000 +00000-0 +00000-0 0 00004
2 15199 3.4709 255.4490 7630028 99.7124 304.9779 1.53318242 05
| Epoch (UTC): | 30 May 2026 12:22:09 |
| Eccentricity: | 0.7630028 |
| inclination: | 3.4709° |
| perigee height: | 1151 km |
| apogee height: | 49631 km |
| right ascension of ascending node: | 255.4490° |
| argument of perigee: | 99.7124° |
| revolutions per day: | 1.53318242 |
| mean anomaly at epoch: | 304.9779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|