View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48300U 26145.28191606 +.00000000 +00000-0 +18339-3 0 00006
2 48300 53.1583 91.9315 0001235 90.7590 269.3553 15.31702566 00
| Epoch (UTC): | 25 May 2026 06:45:57 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 91.9315° |
| argument of perigee: | 90.7590° |
| revolutions per day: | 15.31702566 |
| mean anomaly at epoch: | 269.3553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|