View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00051U 26134.49096750 +.00000000 +00000-0 -12156-3 0 00004
2 00051 47.2094 153.6232 0106164 96.7963 264.4918 12.18377088 03
| Epoch (UTC): | 14 May 2026 11:46:59 |
| Eccentricity: | 0.0106164 |
| inclination: | 47.2094° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 153.6232° |
| argument of perigee: | 96.7963° |
| revolutions per day: | 12.18377088 |
| mean anomaly at epoch: | 264.4918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|