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 67457U 26145.34642424 +.00000000 +00000-0 +69950-3 0 00001
2 67457 43.0054 132.5061 0002688 269.2220 90.8323 15.27607313 02
| Epoch (UTC): | 25 May 2026 08:18:51 |
| Eccentricity: | 0.0002688 |
| inclination: | 43.0054° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 132.5061° |
| argument of perigee: | 269.2220° |
| revolutions per day: | 15.27607313 |
| mean anomaly at epoch: | 90.8323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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