View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66624U 26145.25821360 +.00000000 +00000-0 +55702-3 0 00004
2 66624 53.1602 143.9947 0001124 61.6848 298.4266 15.30212042 08
| Epoch (UTC): | 25 May 2026 06:11:49 |
| Eccentricity: | 0.0001124 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.9947° |
| argument of perigee: | 61.6848° |
| revolutions per day: | 15.30212042 |
| mean anomaly at epoch: | 298.4266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|