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 47993U 26145.43751091 +.00000000 +00000-0 +13631-2 0 00009
2 47993 53.1532 294.0569 0002240 259.1808 100.8948 15.46258926 07
| Epoch (UTC): | 25 May 2026 10:30:00 |
| Eccentricity: | 0.0002240 |
| inclination: | 53.1532° |
| perigee height: | 426 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 294.0569° |
| argument of perigee: | 259.1808° |
| revolutions per day: | 15.46258926 |
| mean anomaly at epoch: | 100.8948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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