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 58400U 26145.62712720 +.00000000 +00000-0 +12202-3 0 00005
2 58400 97.3052 27.8102 0010233 104.8216 255.4155 15.22489588 05
| Epoch (UTC): | 25 May 2026 15:03:03 |
| Eccentricity: | 0.0010233 |
| inclination: | 97.3052° |
| perigee height: | 491 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 27.8102° |
| argument of perigee: | 104.8216° |
| revolutions per day: | 15.22489588 |
| mean anomaly at epoch: | 255.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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