View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18313U 26088.15843373 +.00000000 +00000-0 +18415-4 0 00000
2 18313 82.5623 5.4071 0008895 302.7993 57.2310 13.84303916 00
| Epoch (UTC): | 29 March 2026 03:48:08 |
| Eccentricity: | 0.0008895 |
| inclination: | 82.5623° |
| perigee height: | 942 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 5.4071° |
| argument of perigee: | 302.7993° |
| revolutions per day: | 13.84303916 |
| mean anomaly at epoch: | 57.2310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|