View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68480U 26145.34326278 +.00000000 +00000-0 +26839-3 0 00003
2 68480 97.7610 104.0469 0004012 13.6425 346.4902 14.92761579 09
| Epoch (UTC): | 25 May 2026 08:14:17 |
| Eccentricity: | 0.0004012 |
| inclination: | 97.7610° |
| perigee height: | 587 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 104.0469° |
| argument of perigee: | 13.6425° |
| revolutions per day: | 14.92761579 |
| mean anomaly at epoch: | 346.4902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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