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 67701U 26145.26206698 +.00000000 +00000-0 +66503-3 0 00004
2 67701 97.2826 256.8130 0001060 93.9872 266.1492 15.33458478 05
| Epoch (UTC): | 25 May 2026 06:17:22 |
| Eccentricity: | 0.0001060 |
| inclination: | 97.2826° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.8130° |
| argument of perigee: | 93.9872° |
| revolutions per day: | 15.33458478 |
| mean anomaly at epoch: | 266.1492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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