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 68462U 26145.33307338 +.00000000 +00000-0 +33615-3 0 00008
2 68462 97.4537 104.1473 0004590 99.2038 260.9715 15.18369862 01
| Epoch (UTC): | 25 May 2026 07:59:37 |
| Eccentricity: | 0.0004590 |
| inclination: | 97.4537° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 104.1473° |
| argument of perigee: | 99.2038° |
| revolutions per day: | 15.18369862 |
| mean anomaly at epoch: | 260.9715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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