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 56097U 26145.11414095 +.00000000 +00000-0 +43134-3 0 00001
2 56097 43.0059 42.6774 0001537 236.9065 123.1639 15.27532969 01
| Epoch (UTC): | 25 May 2026 02:44:21 |
| Eccentricity: | 0.0001537 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 42.6774° |
| argument of perigee: | 236.9065° |
| revolutions per day: | 15.27532969 |
| mean anomaly at epoch: | 123.1639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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