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 26075.75485700 +.00000000 +00000-0 -10869-3 0 00006
2 01314 90.2465 4.2158 0030518 168.8080 219.5264 12.91803349 04
| Epoch (UTC): | 16 March 2026 18:06:59 |
| Eccentricity: | 0.0030518 |
| inclination: | 90.2465° |
| perigee height: | 1271 km |
| apogee height: | 1318 km |
| right ascension of ascending node: | 4.2158° |
| argument of perigee: | 168.8080° |
| revolutions per day: | 12.91803349 |
| mean anomaly at epoch: | 219.5264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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