View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00733U 26069.98740222 +.00000000 +00000-0 +11203-3 0 00003
2 00733 99.1224 83.3955 0031977 254.2399 105.5257 14.34020930 07
| Epoch (UTC): | 10 March 2026 23:41:51 |
| Eccentricity: | 0.0031977 |
| inclination: | 99.1224° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 83.3955° |
| argument of perigee: | 254.2399° |
| revolutions per day: | 14.34020930 |
| mean anomaly at epoch: | 105.5257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|