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 65415U 26145.52092242 +.00000000 +00000-0 +33340-3 0 00004
2 65415 53.1591 235.7433 0001258 78.8821 281.2321 15.30198597 01
| Epoch (UTC): | 25 May 2026 12:30:07 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.7433° |
| argument of perigee: | 78.8821° |
| revolutions per day: | 15.30198597 |
| mean anomaly at epoch: | 281.2321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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