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 26106.56895920 +.00000000 +00000-0 +61505-4 0 00008
2 28230 89.8501 51.3481 0003173 99.6963 260.4621 14.83196401 04
| Epoch (UTC): | 16 April 2026 13:39:18 |
| Eccentricity: | 0.0003173 |
| inclination: | 89.8501° |
| perigee height: | 617 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 51.3481° |
| argument of perigee: | 99.6963° |
| revolutions per day: | 14.83196401 |
| mean anomaly at epoch: | 260.4621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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