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 67815U 26145.50731559 +.00000000 +00000-0 +60601-3 0 00009
2 67815 97.2868 333.6018 0002070 94.1943 265.9536 15.33451370 00
| Epoch (UTC): | 25 May 2026 12:10:32 |
| Eccentricity: | 0.0002070 |
| inclination: | 97.2868° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6018° |
| argument of perigee: | 94.1943° |
| revolutions per day: | 15.33451370 |
| mean anomaly at epoch: | 265.9536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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