View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41923U 26044.72571515 +.00000000 +00000-0 +94215-4 0 00006
2 41923 86.4018 140.0751 0002412 95.0323 265.1148 14.34219584 05
| Epoch (UTC): | 13 February 2026 17:25:01 |
| Eccentricity: | 0.0002412 |
| inclination: | 86.4018° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 140.0751° |
| argument of perigee: | 95.0323° |
| revolutions per day: | 14.34219584 |
| mean anomaly at epoch: | 265.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|