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 56125U 26145.51013455 +.00000000 +00000-0 +14267-5 0 00009
2 56125 43.0040 73.5907 0000766 272.1888 87.8876 15.27575156 06
| Epoch (UTC): | 25 May 2026 12:14:35 |
| Eccentricity: | 0.0000766 |
| inclination: | 43.0040° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.5907° |
| argument of perigee: | 272.1888° |
| revolutions per day: | 15.27575156 |
| mean anomaly at epoch: | 87.8876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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