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 65330U 26145.34172118 +.00000000 +00000-0 +41830-3 0 00004
2 65330 53.1577 210.6286 0000920 68.0604 292.0494 15.30204035 00
| Epoch (UTC): | 25 May 2026 08:12:04 |
| Eccentricity: | 0.0000920 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 210.6286° |
| argument of perigee: | 68.0604° |
| revolutions per day: | 15.30204035 |
| mean anomaly at epoch: | 292.0494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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