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 28230U 26066.49223328 +.00000000 +00000-0 +18399-3 0 00004
2 28230 89.8433 52.1206 0002106 80.3544 279.7919 14.83112411 01
| Epoch (UTC): | 07 March 2026 11:48:48 |
| Eccentricity: | 0.0002106 |
| inclination: | 89.8433° |
| perigee height: | 618 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 52.1206° |
| argument of perigee: | 80.3544° |
| revolutions per day: | 14.83112411 |
| mean anomaly at epoch: | 279.7919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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