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 45696U 26145.46164322 +.00000000 +00000-0 +12218-2 0 00005
2 45696 53.1585 52.3427 0003686 106.5767 253.5640 15.33696986 08
| Epoch (UTC): | 25 May 2026 11:04:45 |
| Eccentricity: | 0.0003686 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 52.3427° |
| argument of perigee: | 106.5767° |
| revolutions per day: | 15.33696986 |
| mean anomaly at epoch: | 253.5640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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