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 67108U 26145.27909633 +.00000000 +00000-0 +78774-3 0 00008
2 67108 43.0006 96.1030 0001104 250.6266 109.4466 15.27600273 02
| Epoch (UTC): | 25 May 2026 06:41:53 |
| Eccentricity: | 0.0001104 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.1030° |
| argument of perigee: | 250.6266° |
| revolutions per day: | 15.27600273 |
| mean anomaly at epoch: | 109.4466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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