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 37214U 26145.62287750 +.00000000 +00000-0 +12025-3 0 00008
2 37214 98.9637 191.5403 0021014 250.0183 272.0439 14.14836846 03
| Epoch (UTC): | 25 May 2026 14:56:56 |
| Eccentricity: | 0.0021014 |
| inclination: | 98.9637° |
| perigee height: | 828 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 191.5403° |
| argument of perigee: | 250.0183° |
| revolutions per day: | 14.14836846 |
| mean anomaly at epoch: | 272.0439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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