View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54007U 26145.50206488 +.00000000 +00000-0 +16599-4 0 00004
2 54007 53.2148 228.9386 0001176 87.0427 273.0699 15.08838346 04
| Epoch (UTC): | 25 May 2026 12:02:58 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 228.9386° |
| argument of perigee: | 87.0427° |
| revolutions per day: | 15.08838346 |
| mean anomaly at epoch: | 273.0699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|