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 26374U 26156.87031154 +.00000000 +00000-0 +12591-2 0 00004
2 26374 68.9147 8.1371 0428940 71.7218 293.0084 14.60997234 03
| Epoch (UTC): | 05 June 2026 20:53:14 |
| Eccentricity: | 0.0428940 |
| inclination: | 68.9147° |
| perigee height: | 387 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 8.1371° |
| argument of perigee: | 71.7218° |
| revolutions per day: | 14.60997234 |
| mean anomaly at epoch: | 293.0084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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