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 65617U 26145.50433458 +.00000000 +00000-0 +89523-4 0 00009
2 65617 49.9992 82.3999 0000998 345.9906 14.0943 13.41461438 07
| Epoch (UTC): | 25 May 2026 12:06:14 |
| Eccentricity: | 0.0000998 |
| inclination: | 49.9992° |
| perigee height: | 1103 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 82.3999° |
| argument of perigee: | 345.9906° |
| revolutions per day: | 13.41461438 |
| mean anomaly at epoch: | 14.0943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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