View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 48100U 26145.31190352 +.00000000 +00000-0 -13262-5 0 00008
2 48100 53.1582 156.1068 0001167 76.9393 283.1738 15.31703488 00
| Epoch (UTC): | 25 May 2026 07:29:08 |
| Eccentricity: | 0.0001167 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.1068° |
| argument of perigee: | 76.9393° |
| revolutions per day: | 15.31703488 |
| mean anomaly at epoch: | 283.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|