View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53230U 26145.15886160 +.00000000 +00000-0 -42568-5 0 00000
2 53230 97.4470 206.2575 0001733 128.4755 231.6628 15.05654414 02
| Epoch (UTC): | 25 May 2026 03:48:45 |
| Eccentricity: | 0.0001733 |
| inclination: | 97.4470° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.2575° |
| argument of perigee: | 128.4755° |
| revolutions per day: | 15.05654414 |
| mean anomaly at epoch: | 231.6628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|