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 68464U 26145.62195955 +.00000000 +00000-0 +22659-3 0 00008
2 68464 97.4503 104.3456 0004082 137.1568 222.9985 15.17454115 07
| Epoch (UTC): | 25 May 2026 14:55:37 |
| Eccentricity: | 0.0004082 |
| inclination: | 97.4503° |
| perigee height: | 511 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 104.3456° |
| argument of perigee: | 137.1568° |
| revolutions per day: | 15.17454115 |
| mean anomaly at epoch: | 222.9985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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