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 23489U 26070.52142361 +.00000000 +00000-0 -24963-1 0 00004
2 23489 64.9317 182.6545 0186638 218.0992 222.5078 11.29034018 07
| Epoch (UTC): | 11 March 2026 12:30:51 |
| Eccentricity: | 0.0186638 |
| inclination: | 64.9317° |
| perigee height: | 1858 km |
| apogee height: | 2172 km |
| right ascension of ascending node: | 182.6545° |
| argument of perigee: | 218.0992° |
| revolutions per day: | 11.29034018 |
| mean anomaly at epoch: | 222.5078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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