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 65498U 26145.35512986 +.00000000 +00000-0 +68875-3 0 00009
2 65498 53.1609 275.1984 0000768 72.3969 287.7115 15.30219614 04
| Epoch (UTC): | 25 May 2026 08:31:23 |
| Eccentricity: | 0.0000768 |
| inclination: | 53.1609° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.1984° |
| argument of perigee: | 72.3969° |
| revolutions per day: | 15.30219614 |
| mean anomaly at epoch: | 287.7115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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