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 67614U 26145.28293738 +.00000000 +00000-0 +20887-3 0 00005
2 67614 97.4236 266.2136 0011803 270.8434 89.1442 15.08276043 08
| Epoch (UTC): | 25 May 2026 06:47:25 |
| Eccentricity: | 0.0011803 |
| inclination: | 97.4236° |
| perigee height: | 533 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.2136° |
| argument of perigee: | 270.8434° |
| revolutions per day: | 15.08276043 |
| mean anomaly at epoch: | 89.1442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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