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 65257U 26145.40277162 +.00000000 +00000-0 +42854-3 0 00001
2 65257 97.4489 188.2448 0000828 139.2714 220.8575 15.05658313 04
| Epoch (UTC): | 25 May 2026 09:39:59 |
| Eccentricity: | 0.0000828 |
| inclination: | 97.4489° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 188.2448° |
| argument of perigee: | 139.2714° |
| revolutions per day: | 15.05658313 |
| mean anomaly at epoch: | 220.8575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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