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 36037U 26130.06984299 +.00000000 +00000-0 +39429-4 0 00002
2 36037 98.2451 313.9520 0014107 42.9404 317.2892 14.54846017 01
| Epoch (UTC): | 10 May 2026 01:40:34 |
| Eccentricity: | 0.0014107 |
| inclination: | 98.2451° |
| perigee height: | 700 km |
| apogee height: | 720 km |
| right ascension of ascending node: | 313.9520° |
| argument of perigee: | 42.9404° |
| revolutions per day: | 14.54846017 |
| mean anomaly at epoch: | 317.2892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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