View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60303U 26145.35363544 +.00000000 +00000-0 +17834-4 0 00003
2 60303 53.1597 128.4009 0001204 104.3931 255.7221 15.69705250 00
| Epoch (UTC): | 25 May 2026 08:29:14 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 128.4009° |
| argument of perigee: | 104.3931° |
| revolutions per day: | 15.69705250 |
| mean anomaly at epoch: | 255.7221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|