View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67603U 26145.14067766 +.00000000 +00000-0 +42193-3 0 00002
2 67603 97.2840 210.3167 0000344 342.5488 17.5743 15.33446603 01
| Epoch (UTC): | 25 May 2026 03:22:34 |
| Eccentricity: | 0.0000344 |
| inclination: | 97.2840° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.3167° |
| argument of perigee: | 342.5488° |
| revolutions per day: | 15.33446603 |
| mean anomaly at epoch: | 17.5743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|