View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26069U 26044.71853182 +.00000000 +00000-0 +83421-4 0 00009
2 26069 70.9925 210.2816 0009722 123.7513 236.4537 14.13866683 05
| Epoch (UTC): | 13 February 2026 17:14:41 |
| Eccentricity: | 0.0009722 |
| inclination: | 70.9925° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 210.2816° |
| argument of perigee: | 123.7513° |
| revolutions per day: | 14.13866683 |
| mean anomaly at epoch: | 236.4537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|