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 56903U 26145.65540707 +.00000000 +00000-0 +57738-5 0 00003
2 56903 43.0059 6.9150 0001197 264.1546 95.9170 15.27575642 08
| Epoch (UTC): | 25 May 2026 15:43:47 |
| Eccentricity: | 0.0001197 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.9150° |
| argument of perigee: | 264.1546° |
| revolutions per day: | 15.27575642 |
| mean anomaly at epoch: | 95.9170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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