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 67900U 26145.36863720 +.00000000 +00000-0 +52137-3 0 00009
2 67900 97.2831 78.9576 0002182 93.9011 266.2482 15.33443556 01
| Epoch (UTC): | 25 May 2026 08:50:50 |
| Eccentricity: | 0.0002182 |
| inclination: | 97.2831° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9576° |
| argument of perigee: | 93.9011° |
| revolutions per day: | 15.33443556 |
| mean anomaly at epoch: | 266.2482° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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