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 28932U 26140.36711215 +.00000000 +00000-0 +21812-3 0 00003
2 28932 98.2542 293.6932 0050760 358.8905 1.2206 15.17691944 04
| Epoch (UTC): | 20 May 2026 08:48:38 |
| Eccentricity: | 0.0050760 |
| inclination: | 98.2542° |
| perigee height: | 478 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 293.6932° |
| argument of perigee: | 358.8905° |
| revolutions per day: | 15.17691944 |
| mean anomaly at epoch: | 1.2206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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