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 47935U 26145.64417235 +.00000000 +00000-0 +82098-4 0 00002
2 47935 97.5465 30.7711 0014112 46.2366 314.0022 14.99269969 07
| Epoch (UTC): | 25 May 2026 15:27:36 |
| Eccentricity: | 0.0014112 |
| inclination: | 97.5465° |
| perigee height: | 559 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 30.7711° |
| argument of perigee: | 46.2366° |
| revolutions per day: | 14.99269969 |
| mean anomaly at epoch: | 314.0022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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