View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48377U 26144.99604929 +.00000000 +00000-0 +13323-3 0 00002
2 48377 53.1612 352.9583 0001212 94.6140 265.5000 15.31718529 04
| Epoch (UTC): | 24 May 2026 23:54:18 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 352.9583° |
| argument of perigee: | 94.6140° |
| revolutions per day: | 15.31718529 |
| mean anomaly at epoch: | 265.5000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|