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 68365U 26145.16567272 +.00000000 +00000-0 +38938-3 0 00009
2 68365 82.2982 38.7560 0012422 63.3748 296.8779 15.60761228 08
| Epoch (UTC): | 25 May 2026 03:58:34 |
| Eccentricity: | 0.0012422 |
| inclination: | 82.2982° |
| perigee height: | 377 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 38.7560° |
| argument of perigee: | 63.3748° |
| revolutions per day: | 15.60761228 |
| mean anomaly at epoch: | 296.8779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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