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 59451U 26145.04502728 +.00000000 +00000-0 +35401-3 0 00009
2 59451 45.6076 15.3576 0001595 297.4215 62.6506 15.05570038 00
| Epoch (UTC): | 25 May 2026 01:04:50 |
| Eccentricity: | 0.0001595 |
| inclination: | 45.6076° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 15.3576° |
| argument of perigee: | 297.4215° |
| revolutions per day: | 15.05570038 |
| mean anomaly at epoch: | 62.6506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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