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 67400U 26145.46025413 +.00000000 +00000-0 +69216-3 0 00000
2 67400 97.4560 144.7961 0010596 73.4103 286.8294 15.17783861 07
| Epoch (UTC): | 25 May 2026 11:02:45 |
| Eccentricity: | 0.0010596 |
| inclination: | 97.4560° |
| perigee height: | 505 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 144.7961° |
| argument of perigee: | 73.4103° |
| revolutions per day: | 15.17783861 |
| mean anomaly at epoch: | 286.8294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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