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 26093U 26150.80824845 +.00000000 +00000-0 +66317-3 0 00002
2 26093 100.1904 294.2035 0022664 267.9233 91.9368 14.65123721 02
| Epoch (UTC): | 30 May 2026 19:23:52 |
| Eccentricity: | 0.0022664 |
| inclination: | 100.1904° |
| perigee height: | 661 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 294.2035° |
| argument of perigee: | 267.9233° |
| revolutions per day: | 14.65123721 |
| mean anomaly at epoch: | 91.9368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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