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 26078.07407404 +.00000000 +00000-0 +65477-4 0 00004
2 36037 98.2437 262.6765 0012885 193.9099 166.1745 14.54797792 07
| Epoch (UTC): | 19 March 2026 01:46:39 |
| Eccentricity: | 0.0012885 |
| inclination: | 98.2437° |
| perigee height: | 701 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 262.6765° |
| argument of perigee: | 193.9099° |
| revolutions per day: | 14.54797792 |
| mean anomaly at epoch: | 166.1745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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