View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14051U 26074.29010220 +.00000000 +00000-0 +47827-3 0 00000
2 14051 25.3334 63.6429 0984847 227.2996 124.0343 13.34408074 01
| Epoch (UTC): | 15 March 2026 06:57:44 |
| Eccentricity: | 0.0984847 |
| inclination: | 25.3334° |
| perigee height: | 391 km |
| apogee height: | 1870 km |
| right ascension of ascending node: | 63.6429° |
| argument of perigee: | 227.2996° |
| revolutions per day: | 13.34408074 |
| mean anomaly at epoch: | 124.0343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|