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 47814U 26145.55314419 +.00000000 +00000-0 +10511-3 0 00008
2 47814 53.1580 245.3233 0001035 80.7350 279.3768 15.31704995 08
| Epoch (UTC): | 25 May 2026 13:16:31 |
| Eccentricity: | 0.0001035 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 245.3233° |
| argument of perigee: | 80.7350° |
| revolutions per day: | 15.31704995 |
| mean anomaly at epoch: | 279.3768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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