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 37849U 26047.24532527 +.00000000 +00000-0 +66118-4 0 00009
2 37849 98.7845 349.0218 0001201 2.6442 357.4740 14.19537191 04
| Epoch (UTC): | 16 February 2026 05:53:16 |
| Eccentricity: | 0.0001201 |
| inclination: | 98.7845° |
| perigee height: | 826 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 349.0218° |
| argument of perigee: | 2.6442° |
| revolutions per day: | 14.19537191 |
| mean anomaly at epoch: | 357.4740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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