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 10513U 26039.84672736 +.00000000 +00000-0 +10858-3 0 00001
2 10513 65.8316 195.1791 0036502 275.5752 195.6394 13.78860274 06
| Epoch (UTC): | 08 February 2026 20:19:17 |
| Eccentricity: | 0.0036502 |
| inclination: | 65.8316° |
| perigee height: | 941 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 195.1791° |
| argument of perigee: | 275.5752° |
| revolutions per day: | 13.78860274 |
| mean anomaly at epoch: | 195.6394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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