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 68487U 26145.35499769 +.00000000 +00000-0 +38280-3 0 00000
2 68487 97.7528 103.9783 0001679 30.0181 330.1135 14.92479068 06
| Epoch (UTC): | 25 May 2026 08:31:11 |
| Eccentricity: | 0.0001679 |
| inclination: | 97.7528° |
| perigee height: | 589 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 103.9783° |
| argument of perigee: | 30.0181° |
| revolutions per day: | 14.92479068 |
| mean anomaly at epoch: | 330.1135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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