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 01314U 26029.90693162 +.00000000 +00000-0 +80895-4 0 00001
2 01314 90.2397 3.2054 0028716 292.9543 119.6142 12.91802712 00
| Epoch (UTC): | 29 January 2026 21:45:58 |
| Eccentricity: | 0.0028716 |
| inclination: | 90.2397° |
| perigee height: | 1272 km |
| apogee height: | 1316 km |
| right ascension of ascending node: | 3.2054° |
| argument of perigee: | 292.9543° |
| revolutions per day: | 12.91802712 |
| mean anomaly at epoch: | 119.6142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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