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 51947U 26145.63366132 +.00000000 +00000-0 +60919-3 0 00005
2 51947 63.4846 346.3710 0098238 347.2786 12.5849 15.18000378 02
| Epoch (UTC): | 25 May 2026 15:12:28 |
| Eccentricity: | 0.0098238 |
| inclination: | 63.4846° |
| perigee height: | 444 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 346.3710° |
| argument of perigee: | 347.2786° |
| revolutions per day: | 15.18000378 |
| mean anomaly at epoch: | 12.5849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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