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 58712U 26145.21161236 +.00000000 +00000-0 +41387-4 0 00003
2 58712 53.1616 234.3260 0000563 92.2823 267.8242 15.30195720 01
| Epoch (UTC): | 25 May 2026 05:04:43 |
| Eccentricity: | 0.0000563 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.3260° |
| argument of perigee: | 92.2823° |
| revolutions per day: | 15.30195720 |
| mean anomaly at epoch: | 267.8242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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