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 47800U 26145.54264177 +.00000000 +00000-0 +45166-5 0 00003
2 47800 53.1582 241.6057 0000870 91.2395 268.8706 15.31706911 05
| Epoch (UTC): | 25 May 2026 13:01:24 |
| Eccentricity: | 0.0000870 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 241.6057° |
| argument of perigee: | 91.2395° |
| revolutions per day: | 15.31706911 |
| mean anomaly at epoch: | 268.8706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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