View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45415U 26065.21287971 +.00000000 +00000-0 -62002-5 0 00004
2 45415 53.1618 145.4470 0001934 126.2260 233.8920 15.30186173 08
| Epoch (UTC): | 06 March 2026 05:06:32 |
| Eccentricity: | 0.0001934 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 145.4470° |
| argument of perigee: | 126.2260° |
| revolutions per day: | 15.30186173 |
| mean anomaly at epoch: | 233.8920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|