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 26103.88786711 +.00000000 +00000-0 +36711-3 0 00001
2 02674 39.9167 296.3595 0205266 167.1541 193.4578 14.74207137 04
| Epoch (UTC): | 13 April 2026 21:18:31 |
| Eccentricity: | 0.0205266 |
| inclination: | 39.9167° |
| perigee height: | 503 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 296.3595° |
| argument of perigee: | 167.1541° |
| revolutions per day: | 14.74207137 |
| mean anomaly at epoch: | 193.4578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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