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 67133U 26145.52712843 +.00000000 +00000-0 +32300-3 0 00004
2 67133 51.9011 75.5755 0001121 55.4890 304.6177 14.76425883 05
| Epoch (UTC): | 25 May 2026 12:39:03 |
| Eccentricity: | 0.0001121 |
| inclination: | 51.9011° |
| perigee height: | 640 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 75.5755° |
| argument of perigee: | 55.4890° |
| revolutions per day: | 14.76425883 |
| mean anomaly at epoch: | 304.6177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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