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 68430U 26145.38632434 +.00000000 +00000-0 +31220-3 0 00006
2 68430 97.4481 104.1887 0002607 81.5593 278.5937 15.18697252 08
| Epoch (UTC): | 25 May 2026 09:16:18 |
| Eccentricity: | 0.0002607 |
| inclination: | 97.4481° |
| perigee height: | 508 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 104.1887° |
| argument of perigee: | 81.5593° |
| revolutions per day: | 15.18697252 |
| mean anomaly at epoch: | 278.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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