View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43752U 26145.61880634 +.00000000 +00000-0 -65781-3 0 00009
2 43752 82.5192 237.3361 0018015 104.7496 255.5582 12.42912076 07
| Epoch (UTC): | 25 May 2026 14:51:04 |
| Eccentricity: | 0.0018015 |
| inclination: | 82.5192° |
| perigee height: | 1480 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 237.3361° |
| argument of perigee: | 104.7496° |
| revolutions per day: | 12.42912076 |
| mean anomaly at epoch: | 255.5582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|