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 68516U 26145.36627653 +.00000000 +00000-0 +11529-2 0 00005
2 68516 53.1599 131.7447 0001323 90.0330 270.0824 15.34390942 04
| Epoch (UTC): | 25 May 2026 08:47:26 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 131.7447° |
| argument of perigee: | 90.0330° |
| revolutions per day: | 15.34390942 |
| mean anomaly at epoch: | 270.0824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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