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 60576U 26145.20476757 +.00000000 +00000-0 +67343-3 0 00009
2 60576 97.6994 230.0000 0003440 93.1624 267.0000 15.12094459 06
| Epoch (UTC): | 25 May 2026 04:54:51 |
| Eccentricity: | 0.0003440 |
| inclination: | 97.6994° |
| perigee height: | 527 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 230.0000° |
| argument of perigee: | 93.1624° |
| revolutions per day: | 15.12094459 |
| mean anomaly at epoch: | 267.0000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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