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 28414U 26042.26585365 +.00000000 +00000-0 +24431-3 0 00003
2 28414 97.6156 61.7652 0004243 195.5705 164.5392 15.05506272 00
| Epoch (UTC): | 11 February 2026 06:22:49 |
| Eccentricity: | 0.0004243 |
| inclination: | 97.6156° |
| perigee height: | 547 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 61.7652° |
| argument of perigee: | 195.5705° |
| revolutions per day: | 15.05506272 |
| mean anomaly at epoch: | 164.5392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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