View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02986U 26088.20050203 +.00000000 +00000-0 +24598-3 0 00005
2 02986 90.4800 188.1238 0047668 119.0334 241.5636 14.06505262 09
| Epoch (UTC): | 29 March 2026 04:48:43 |
| Eccentricity: | 0.0047668 |
| inclination: | 90.4800° |
| perigee height: | 837 km |
| apogee height: | 906 km |
| right ascension of ascending node: | 188.1238° |
| argument of perigee: | 119.0334° |
| revolutions per day: | 14.06505262 |
| mean anomaly at epoch: | 241.5636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|