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 26079.44964861 +.00000000 +00000-0 +62572-4 0 00004
2 36037 98.2438 264.0329 0012980 189.6068 170.4883 14.54798461 09
| Epoch (UTC): | 20 March 2026 10:47:29 |
| Eccentricity: | 0.0012980 |
| inclination: | 98.2438° |
| perigee height: | 701 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 264.0329° |
| argument of perigee: | 189.6068° |
| revolutions per day: | 14.54798461 |
| mean anomaly at epoch: | 170.4883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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