View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48309U 26145.55513063 +.00000000 +00000-0 +46302-5 0 00003
2 48309 53.1586 91.1143 0001370 90.2641 269.8517 15.30194303 03
| Epoch (UTC): | 25 May 2026 13:19:23 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.1143° |
| argument of perigee: | 90.2641° |
| revolutions per day: | 15.30194303 |
| mean anomaly at epoch: | 269.8517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|