View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65287U 26145.42132932 +.00000000 +00000-0 +36136-3 0 00007
2 65287 97.4483 197.8753 0001481 136.7876 223.3467 15.05657439 09
| Epoch (UTC): | 25 May 2026 10:06:42 |
| Eccentricity: | 0.0001481 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8753° |
| argument of perigee: | 136.7876° |
| revolutions per day: | 15.05657439 |
| mean anomaly at epoch: | 223.3467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|