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 68694U 26145.64602345 +.00000000 +00000-0 +31254-3 0 00002
2 68694 97.6660 221.2816 0020656 130.9475 229.3545 15.08779591 01
| Epoch (UTC): | 25 May 2026 15:30:16 |
| Eccentricity: | 0.0020656 |
| inclination: | 97.6660° |
| perigee height: | 526 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 221.2816° |
| argument of perigee: | 130.9475° |
| revolutions per day: | 15.08779591 |
| mean anomaly at epoch: | 229.3545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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