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 28650U 26155.06544815 +.00000000 +00000-0 +37820-3 0 00009
2 28650 97.9909 177.5802 0020868 82.6739 277.6859 15.09605835 01
| Epoch (UTC): | 04 June 2026 01:34:14 |
| Eccentricity: | 0.0020868 |
| inclination: | 97.9909° |
| perigee height: | 523 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 177.5802° |
| argument of perigee: | 82.6739° |
| revolutions per day: | 15.09605835 |
| mean anomaly at epoch: | 277.6859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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