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 68514U 26145.26588788 +.00000000 +00000-0 +11111-2 0 00004
2 68514 53.1572 133.2767 0001153 77.0067 283.1068 15.42178854 08
| Epoch (UTC): | 25 May 2026 06:22:52 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1572° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 133.2767° |
| argument of perigee: | 77.0067° |
| revolutions per day: | 15.42178854 |
| mean anomaly at epoch: | 283.1068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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