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 67994U 26145.25821591 +.00000000 +00000-0 +66187-3 0 00000
2 67994 43.0035 336.5046 0001473 267.4044 92.6639 15.27592378 05
| Epoch (UTC): | 25 May 2026 06:11:49 |
| Eccentricity: | 0.0001473 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 336.5046° |
| argument of perigee: | 267.4044° |
| revolutions per day: | 15.27592378 |
| mean anomaly at epoch: | 92.6639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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