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 68463U 26145.62179233 +.00000000 +00000-0 +32332-3 0 00007
2 68463 97.4520 104.3602 0004947 127.7503 232.4179 15.17501880 05
| Epoch (UTC): | 25 May 2026 14:55:22 |
| Eccentricity: | 0.0004947 |
| inclination: | 97.4520° |
| perigee height: | 510 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 104.3602° |
| argument of perigee: | 127.7503° |
| revolutions per day: | 15.17501880 |
| mean anomaly at epoch: | 232.4179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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