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 26041.87986865 +.00000000 +00000-0 +78855-4 0 00000
2 10513 65.8320 190.1233 0036499 274.8146 207.6947 13.78860411 02
| Epoch (UTC): | 10 February 2026 21:07:00 |
| Eccentricity: | 0.0036499 |
| inclination: | 65.8320° |
| perigee height: | 941 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 190.1233° |
| argument of perigee: | 274.8146° |
| revolutions per day: | 13.78860411 |
| mean anomaly at epoch: | 207.6947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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