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 65916U 26145.47641498 +.00000000 +00000-0 +80282-3 0 00004
2 65916 53.1587 169.0768 0000982 83.8075 276.3038 15.30203367 04
| Epoch (UTC): | 25 May 2026 11:26:02 |
| Eccentricity: | 0.0000982 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0768° |
| argument of perigee: | 83.8075° |
| revolutions per day: | 15.30203367 |
| mean anomaly at epoch: | 276.3038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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