View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37849U 26032.51391728 +.00000000 +00000-0 +66501-4 0 00005
2 37849 98.7829 334.4132 0001911 32.9457 327.1838 14.19532351 04
| Epoch (UTC): | 01 February 2026 12:20:02 |
| Eccentricity: | 0.0001911 |
| inclination: | 98.7829° |
| perigee height: | 826 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 334.4132° |
| argument of perigee: | 32.9457° |
| revolutions per day: | 14.19532351 |
| mean anomaly at epoch: | 327.1838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|