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 67137U 26145.59579517 +.00000000 +00000-0 +13849-3 0 00001
2 67137 51.9000 98.0353 0001663 79.4792 280.6358 14.79947415 06
| Epoch (UTC): | 25 May 2026 14:17:56 |
| Eccentricity: | 0.0001663 |
| inclination: | 51.9000° |
| perigee height: | 628 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 98.0353° |
| argument of perigee: | 79.4792° |
| revolutions per day: | 14.79947415 |
| mean anomaly at epoch: | 280.6358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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