View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 23088U 26073.38057291 +.00000000 +00000-0 -63894-4 0 00002
2 23088 70.9984 61.0340 0005648 280.9015 79.1472 14.15010387 02
| Epoch (UTC): | 14 March 2026 09:08:01 |
| Eccentricity: | 0.0005648 |
| inclination: | 70.9984° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 61.0340° |
| argument of perigee: | 280.9015° |
| revolutions per day: | 14.15010387 |
| mean anomaly at epoch: | 79.1472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|