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 47798U 26145.01132691 +.00000000 +00000-0 +75809-4 0 00002
2 47798 53.1580 244.1670 0001549 85.3858 274.7320 15.31712039 06
| Epoch (UTC): | 25 May 2026 00:16:18 |
| Eccentricity: | 0.0001549 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 244.1670° |
| argument of perigee: | 85.3858° |
| revolutions per day: | 15.31712039 |
| mean anomaly at epoch: | 274.7320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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