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 56703U 26145.44415172 +.00000000 +00000-0 +19257-6 0 00000
2 56703 43.0004 200.5696 0001237 269.2946 90.7764 15.27576797 02
| Epoch (UTC): | 25 May 2026 10:39:34 |
| Eccentricity: | 0.0001237 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.5696° |
| argument of perigee: | 269.2946° |
| revolutions per day: | 15.27576797 |
| mean anomaly at epoch: | 90.7764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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