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 28892U 26104.16722946 +.00000000 +00000-0 +14656-3 0 00007
2 28892 98.2988 259.0362 0014724 56.6435 303.6178 14.71956598 02
| Epoch (UTC): | 14 April 2026 04:00:48 |
| Eccentricity: | 0.0014724 |
| inclination: | 98.2988° |
| perigee height: | 644 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 259.0362° |
| argument of perigee: | 56.6435° |
| revolutions per day: | 14.71956598 |
| mean anomaly at epoch: | 303.6178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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