View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46913U 26145.60005043 +.00000000 +00000-0 +27251-3 0 00002
2 46913 36.8966 200.4384 0006052 94.7424 265.4016 15.25063389 03
| Epoch (UTC): | 25 May 2026 14:24:04 |
| Eccentricity: | 0.0006052 |
| inclination: | 36.8966° |
| perigee height: | 486 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 200.4384° |
| argument of perigee: | 94.7424° |
| revolutions per day: | 15.25063389 |
| mean anomaly at epoch: | 265.4016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|