View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41167U 26145.43874486 +.00000000 +00000-0 +12555-3 0 00005
2 41167 14.9801 75.1395 0008447 278.0603 81.8761 15.22970184 03
| Epoch (UTC): | 25 May 2026 10:31:47 |
| Eccentricity: | 0.0008447 |
| inclination: | 14.9801° |
| perigee height: | 491 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 75.1395° |
| argument of perigee: | 278.0603° |
| revolutions per day: | 15.22970184 |
| mean anomaly at epoch: | 81.8761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|