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 25774U 26071.87818650 +.00000000 +00000-0 +73068-4 0 00005
2 25774 51.5282 244.3085 0373972 254.5986 272.1264 13.46767796 06
| Epoch (UTC): | 12 March 2026 21:04:35 |
| Eccentricity: | 0.0373972 |
| inclination: | 51.5282° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 244.3085° |
| argument of perigee: | 254.5986° |
| revolutions per day: | 13.46767796 |
| mean anomaly at epoch: | 272.1264° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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