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 37187U 26072.68756624 +.00000000 +00000-0 +16563-2 0 00003
2 37187 49.5404 230.2094 5099736 141.5258 269.1245 5.40515998 04
| Epoch (UTC): | 13 March 2026 16:30:05 |
| Eccentricity: | 0.5099736 |
| inclination: | 49.5404° |
| perigee height: | 343 km |
| apogee height: | 14331 km |
| right ascension of ascending node: | 230.2094° |
| argument of perigee: | 141.5258° |
| revolutions per day: | 5.40515998 |
| mean anomaly at epoch: | 269.1245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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