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 68887U 26145.58335647 +.00000000 +00000-0 +92609-3 0 00008
2 68887 51.8853 351.4587 0001088 95.6387 308.1245 15.37325797 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001088 |
| inclination: | 51.8853° |
| perigee height: | 453 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 351.4587° |
| argument of perigee: | 95.6387° |
| revolutions per day: | 15.37325797 |
| mean anomaly at epoch: | 308.1245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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