View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67664U 26145.06824628 +.00000000 +00000-0 +55765-3 0 00007
2 67664 97.2841 178.2590 0001434 78.1070 282.0333 15.33449717 04
| Epoch (UTC): | 25 May 2026 01:38:16 |
| Eccentricity: | 0.0001434 |
| inclination: | 97.2841° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 178.2590° |
| argument of perigee: | 78.1070° |
| revolutions per day: | 15.33449717 |
| mean anomaly at epoch: | 282.0333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|