View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27387U 26072.99012817 +.00000000 +00000-0 +52346-4 0 00008
2 27387 98.8154 88.9025 0032883 48.4918 311.9081 14.36772588 08
| Epoch (UTC): | 13 March 2026 23:45:47 |
| Eccentricity: | 0.0032883 |
| inclination: | 98.8154° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 88.9025° |
| argument of perigee: | 48.4918° |
| revolutions per day: | 14.36772588 |
| mean anomaly at epoch: | 311.9081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|