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 39484U 26118.82893747 +.00000000 +00000-0 -83052-3 0 00009
2 39484 82.4910 200.8051 0021174 199.6861 160.3404 12.42878426 07
| Epoch (UTC): | 28 April 2026 19:53:40 |
| Eccentricity: | 0.0021174 |
| inclination: | 82.4910° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 200.8051° |
| argument of perigee: | 199.6861° |
| revolutions per day: | 12.42878426 |
| mean anomaly at epoch: | 160.3404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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