View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12848U 26160.29514190 +.00000000 +00000-0 +35339-3 0 00008
2 12848 82.4643 295.3045 0459998 222.5528 133.9171 14.58626426 09
| Epoch (UTC): | 09 June 2026 07:05:00 |
| Eccentricity: | 0.0459998 |
| inclination: | 82.4643° |
| perigee height: | 372 km |
| apogee height: | 1023 km |
| right ascension of ascending node: | 295.3045° |
| argument of perigee: | 222.5528° |
| revolutions per day: | 14.58626426 |
| mean anomaly at epoch: | 133.9171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|