View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48287U 26145.23291455 +.00000000 +00000-0 +80694-4 0 00002
2 48287 53.1593 81.8059 0001180 94.9617 265.1519 15.31704901 04
| Epoch (UTC): | 25 May 2026 05:35:23 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 81.8059° |
| argument of perigee: | 94.9617° |
| revolutions per day: | 15.31704901 |
| mean anomaly at epoch: | 265.1519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|