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 54249U 26145.64642014 +.00000000 +00000-0 +66601-4 0 00005
2 54249 63.4070 320.0828 0074479 355.3795 4.6535 13.45439203 04
| Epoch (UTC): | 25 May 2026 15:30:50 |
| Eccentricity: | 0.0074479 |
| inclination: | 63.4070° |
| perigee height: | 1033 km |
| apogee height: | 1145 km |
| right ascension of ascending node: | 320.0828° |
| argument of perigee: | 355.3795° |
| revolutions per day: | 13.45439203 |
| mean anomaly at epoch: | 4.6535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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