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 65151U 26145.43997378 +.00000000 +00000-0 +51742-4 0 00002
2 65151 51.8971 196.2086 0000347 87.6335 272.4667 14.79932420 04
| Epoch (UTC): | 25 May 2026 10:33:33 |
| Eccentricity: | 0.0000347 |
| inclination: | 51.8971° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 196.2086° |
| argument of perigee: | 87.6335° |
| revolutions per day: | 14.79932420 |
| mean anomaly at epoch: | 272.4667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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