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 68432U 26145.33285470 +.00000000 +00000-0 +24572-3 0 00009
2 68432 97.4542 104.1489 0004372 97.0497 263.1235 15.18292941 09
| Epoch (UTC): | 25 May 2026 07:59:18 |
| Eccentricity: | 0.0004372 |
| inclination: | 97.4542° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 104.1489° |
| argument of perigee: | 97.0497° |
| revolutions per day: | 15.18292941 |
| mean anomaly at epoch: | 263.1235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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