View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63553U 26145.13379036 +.00000000 +00000-0 +12153-2 0 00009
2 63553 42.9973 52.8077 0000661 140.2496 219.8420 15.70983748 04
| Epoch (UTC): | 25 May 2026 03:12:39 |
| Eccentricity: | 0.0000661 |
| inclination: | 42.9973° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 52.8077° |
| argument of perigee: | 140.2496° |
| revolutions per day: | 15.70983748 |
| mean anomaly at epoch: | 219.8420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|