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 61878U 26144.84674647 +.00000000 +00000-0 +15790-4 0 00002
2 61878 53.1595 341.0057 0000991 75.5518 284.5610 15.69708080 00
| Epoch (UTC): | 24 May 2026 20:19:18 |
| Eccentricity: | 0.0000991 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 341.0057° |
| argument of perigee: | 75.5518° |
| revolutions per day: | 15.69708080 |
| mean anomaly at epoch: | 284.5610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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