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 67144U 26145.15081830 +.00000000 +00000-0 +65795-3 0 00004
2 67144 51.8774 55.1633 0001395 251.8413 108.2418 15.28443826 08
| Epoch (UTC): | 25 May 2026 03:37:10 |
| Eccentricity: | 0.0001395 |
| inclination: | 51.8774° |
| perigee height: | 480 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 55.1633° |
| argument of perigee: | 251.8413° |
| revolutions per day: | 15.28443826 |
| mean anomaly at epoch: | 108.2418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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