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 67187U 26145.55629781 +.00000000 +00000-0 +88188-3 0 00009
2 67187 42.9999 236.3704 0001110 292.0531 68.0203 15.27594582 00
| Epoch (UTC): | 25 May 2026 13:21:04 |
| Eccentricity: | 0.0001110 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.3704° |
| argument of perigee: | 292.0531° |
| revolutions per day: | 15.27594582 |
| mean anomaly at epoch: | 68.0203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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