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 68461U 26145.35364875 +.00000000 +00000-0 +35479-3 0 00008
2 68461 97.4534 104.1186 0005302 126.8985 233.2735 15.17806395 09
| Epoch (UTC): | 25 May 2026 08:29:15 |
| Eccentricity: | 0.0005302 |
| inclination: | 97.4534° |
| perigee height: | 509 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 104.1186° |
| argument of perigee: | 126.8985° |
| revolutions per day: | 15.17806395 |
| mean anomaly at epoch: | 233.2735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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