View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27386U 26064.31924942 +.00000000 +00000-0 +77384-4 0 00004
2 27386 98.3722 18.0208 0001332 84.4515 70.7498 14.39035096 09
| Epoch (UTC): | 05 March 2026 07:39:43 |
| Eccentricity: | 0.0001332 |
| inclination: | 98.3722° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 18.0208° |
| argument of perigee: | 84.4515° |
| revolutions per day: | 14.39035096 |
| mean anomaly at epoch: | 70.7498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|