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 02674U 26106.80072428 +.00000000 +00000-0 +39963-3 0 00001
2 02674 39.9167 280.4598 0205667 187.2678 172.5105 14.74227262 05
| Epoch (UTC): | 16 April 2026 19:13:02 |
| Eccentricity: | 0.0205667 |
| inclination: | 39.9167° |
| perigee height: | 503 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 280.4598° |
| argument of perigee: | 187.2678° |
| revolutions per day: | 14.74227262 |
| mean anomaly at epoch: | 172.5105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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