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 65652U 26145.08569168 +.00000000 +00000-0 +28632-3 0 00002
2 65652 97.4494 188.9456 0001977 182.3762 177.7456 15.05648350 01
| Epoch (UTC): | 25 May 2026 02:03:23 |
| Eccentricity: | 0.0001977 |
| inclination: | 97.4494° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.9456° |
| argument of perigee: | 182.3762° |
| revolutions per day: | 15.05648350 |
| mean anomaly at epoch: | 177.7456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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