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 68087U 26145.53628619 +.00000000 +00000-0 +10898-2 0 00008
2 68087 53.1577 180.8459 0001247 91.7558 268.3588 15.34444629 05
| Epoch (UTC): | 25 May 2026 12:52:15 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.1577° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 180.8459° |
| argument of perigee: | 91.7558° |
| revolutions per day: | 15.34444629 |
| mean anomaly at epoch: | 268.3588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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