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 67972U 26145.45346052 +.00000000 +00000-0 +48771-3 0 00001
2 67972 97.2844 155.4806 0001139 66.3444 293.7918 15.33459279 04
| Epoch (UTC): | 25 May 2026 10:52:58 |
| Eccentricity: | 0.0001139 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4806° |
| argument of perigee: | 66.3444° |
| revolutions per day: | 15.33459279 |
| mean anomaly at epoch: | 293.7918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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