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 37756U 26072.97191110 +.00000000 +00000-0 +73727-3 0 00006
2 37756 51.4401 354.6036 1812399 184.3557 173.9332 11.46831042 06
| Epoch (UTC): | 13 March 2026 23:19:33 |
| Eccentricity: | 0.1812399 |
| inclination: | 51.4401° |
| perigee height: | 423 km |
| apogee height: | 3433 km |
| right ascension of ascending node: | 354.6036° |
| argument of perigee: | 184.3557° |
| revolutions per day: | 11.46831042 |
| mean anomaly at epoch: | 173.9332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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