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 56838U 26145.50225676 +.00000000 +00000-0 +87118-4 0 00003
2 56838 43.0003 320.1447 0001225 272.0600 88.0111 15.27585685 01
| Epoch (UTC): | 25 May 2026 12:03:14 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.1447° |
| argument of perigee: | 272.0600° |
| revolutions per day: | 15.27585685 |
| mean anomaly at epoch: | 88.0111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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