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 28485U 26150.55849721 +.00000000 +00000-0 +51528-3 0 00009
2 28485 20.5548 320.7054 0003379 59.3763 300.7015 15.66499139 08
| Epoch (UTC): | 30 May 2026 13:24:14 |
| Eccentricity: | 0.0003379 |
| inclination: | 20.5548° |
| perigee height: | 367 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 320.7054° |
| argument of perigee: | 59.3763° |
| revolutions per day: | 15.66499139 |
| mean anomaly at epoch: | 300.7015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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