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 67875U 26145.43606229 +.00000000 +00000-0 +54230-3 0 00003
2 67875 53.1591 207.2066 0001084 61.3438 298.7672 15.31718740 08
| Epoch (UTC): | 25 May 2026 10:27:55 |
| Eccentricity: | 0.0001084 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 207.2066° |
| argument of perigee: | 61.3438° |
| revolutions per day: | 15.31718740 |
| mean anomaly at epoch: | 298.7672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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