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 67984U 26145.48880846 +.00000000 +00000-0 +57847-3 0 00005
2 67984 97.2832 155.5849 0001359 87.2648 272.8750 15.33456889 00
| Epoch (UTC): | 25 May 2026 11:43:53 |
| Eccentricity: | 0.0001359 |
| inclination: | 97.2832° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5849° |
| argument of perigee: | 87.2648° |
| revolutions per day: | 15.33456889 |
| mean anomaly at epoch: | 272.8750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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