View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 51987U 26145.15572510 +.00000000 +00000-0 +61380-5 0 00000
2 51987 53.2129 55.8499 0001257 83.9544 276.1592 15.08841683 08
| Epoch (UTC): | 25 May 2026 03:44:14 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.8499° |
| argument of perigee: | 83.9544° |
| revolutions per day: | 15.08841683 |
| mean anomaly at epoch: | 276.1592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|