View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39453U 26031.88227250 +.00000000 +00000-0 +20551-3 0 00009
2 39453 87.3348 105.3630 0002842 93.6298 266.5286 15.47863841 02
| Epoch (UTC): | 31 January 2026 21:10:28 |
| Eccentricity: | 0.0002842 |
| inclination: | 87.3348° |
| perigee height: | 421 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 105.3630° |
| argument of perigee: | 93.6298° |
| revolutions per day: | 15.47863841 |
| mean anomaly at epoch: | 266.5286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|