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 65603U 26145.44608846 +.00000000 +00000-0 +14576-3 0 00007
2 65603 97.4460 213.9889 0002304 146.2616 213.8758 15.05655680 02
| Epoch (UTC): | 25 May 2026 10:42:22 |
| Eccentricity: | 0.0002304 |
| inclination: | 97.4460° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.9889° |
| argument of perigee: | 146.2616° |
| revolutions per day: | 15.05655680 |
| mean anomaly at epoch: | 213.8758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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