View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48795U 26145.58190260 +.00000000 +00000-0 +11804-4 0 00003
2 48795 87.8990 263.7394 0001602 98.0657 262.0655 13.15547308 07
| Epoch (UTC): | 25 May 2026 13:57:56 |
| Eccentricity: | 0.0001602 |
| inclination: | 87.8990° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7394° |
| argument of perigee: | 98.0657° |
| revolutions per day: | 13.15547308 |
| mean anomaly at epoch: | 262.0655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|