View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 03338U 26106.54468700 +.00000000 +00000-0 +74312-4 0 00000
2 03338 80.6580 134.0585 1130385 66.7431 304.8499 12.23563143 07
| Epoch (UTC): | 16 April 2026 13:04:20 |
| Eccentricity: | 0.1130385 |
| inclination: | 80.6580° |
| perigee height: | 678 km |
| apogee height: | 2476 km |
| right ascension of ascending node: | 134.0585° |
| argument of perigee: | 66.7431° |
| revolutions per day: | 12.23563143 |
| mean anomaly at epoch: | 304.8499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|