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 65137U 26145.52097741 +.00000000 +00000-0 +29485-3 0 00009
2 65137 51.8993 183.3441 0000324 65.2788 294.8208 14.79943236 09
| Epoch (UTC): | 25 May 2026 12:30:12 |
| Eccentricity: | 0.0000324 |
| inclination: | 51.8993° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 183.3441° |
| argument of perigee: | 65.2788° |
| revolutions per day: | 14.79943236 |
| mean anomaly at epoch: | 294.8208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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