View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 01521U 26137.24812049 +.00000000 +00000-0 +55951-4 0 00000
2 01521 90.0230 210.2346 0069044 351.5377 71.1300 13.33282773 08
| Epoch (UTC): | 17 May 2026 05:57:17 |
| Eccentricity: | 0.0069044 |
| inclination: | 90.0230° |
| perigee height: | 1083 km |
| apogee height: | 1186 km |
| right ascension of ascending node: | 210.2346° |
| argument of perigee: | 351.5377° |
| revolutions per day: | 13.33282773 |
| mean anomaly at epoch: | 71.1300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|