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 56469U 26145.39208580 +.00000000 +00000-0 +90308-5 0 00001
2 56469 69.9989 291.2579 0002920 268.0521 92.0303 14.98329887 00
| Epoch (UTC): | 25 May 2026 09:24:36 |
| Eccentricity: | 0.0002920 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.2579° |
| argument of perigee: | 268.0521° |
| revolutions per day: | 14.98329887 |
| mean anomaly at epoch: | 92.0303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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