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 60209U 26145.49092103 +.00000000 +00000-0 +58166-3 0 00005
2 60209 97.2333 2.4954 0008136 301.4584 58.5878 15.60560579 08
| Epoch (UTC): | 25 May 2026 11:46:55 |
| Eccentricity: | 0.0008136 |
| inclination: | 97.2333° |
| perigee height: | 381 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 2.4954° |
| argument of perigee: | 301.4584° |
| revolutions per day: | 15.60560579 |
| mean anomaly at epoch: | 58.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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