View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27598U 26104.20584045 +.00000000 +00000-0 +42124-4 0 00002
2 27598 98.8552 76.5508 0009282 157.7105 202.4482 14.29713316 07
| Epoch (UTC): | 14 April 2026 04:56:24 |
| Eccentricity: | 0.0009282 |
| inclination: | 98.8552° |
| perigee height: | 786 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 76.5508° |
| argument of perigee: | 157.7105° |
| revolutions per day: | 14.29713316 |
| mean anomaly at epoch: | 202.4482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|