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 00059U 26140.03519258 +.00000000 +00000-0 +31852-4 0 00006
2 00059 28.2482 268.1806 0188892 79.4642 282.7124 13.53168406 04
| Epoch (UTC): | 20 May 2026 00:50:40 |
| Eccentricity: | 0.0188892 |
| inclination: | 28.2482° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 268.1806° |
| argument of perigee: | 79.4642° |
| revolutions per day: | 13.53168406 |
| mean anomaly at epoch: | 282.7124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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