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 26129.10697502 +.00000000 +00000-0 +45351-4 0 00004
2 36037 98.2451 313.0025 0014158 45.7242 314.5114 14.54845784 06
| Epoch (UTC): | 09 May 2026 02:34:02 |
| Eccentricity: | 0.0014158 |
| inclination: | 98.2451° |
| perigee height: | 700 km |
| apogee height: | 720 km |
| right ascension of ascending node: | 313.0025° |
| argument of perigee: | 45.7242° |
| revolutions per day: | 14.54845784 |
| mean anomaly at epoch: | 314.5114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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