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 68494U 26145.38751797 +.00000000 +00000-0 +20995-3 0 00007
2 68494 97.7600 103.9790 0003800 93.7118 266.4536 14.91537460 03
| Epoch (UTC): | 25 May 2026 09:18:01 |
| Eccentricity: | 0.0003800 |
| inclination: | 97.7600° |
| perigee height: | 590 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 103.9790° |
| argument of perigee: | 93.7118° |
| revolutions per day: | 14.91537460 |
| mean anomaly at epoch: | 266.4536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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