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 67383U 26145.46623322 +.00000000 +00000-0 +72205-4 0 00006
2 67383 97.8007 144.3776 0003473 173.8621 186.2638 14.86304440 05
| Epoch (UTC): | 25 May 2026 11:11:22 |
| Eccentricity: | 0.0003473 |
| inclination: | 97.8007° |
| perigee height: | 607 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 144.3776° |
| argument of perigee: | 173.8621° |
| revolutions per day: | 14.86304440 |
| mean anomaly at epoch: | 186.2638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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