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 59921U 26145.34212193 +.00000000 +00000-0 +37423-5 0 00006
2 59921 97.5805 162.0835 0014287 267.9770 91.9827 15.16430288 01
| Epoch (UTC): | 25 May 2026 08:12:39 |
| Eccentricity: | 0.0014287 |
| inclination: | 97.5805° |
| perigee height: | 507 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 162.0835° |
| argument of perigee: | 267.9770° |
| revolutions per day: | 15.16430288 |
| mean anomaly at epoch: | 91.9827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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