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 41900U 26145.45685130 +.00000000 +00000-0 +12998-3 0 00009
2 41900 98.5481 139.2417 0024396 32.9707 327.3008 14.59757594 09
| Epoch (UTC): | 25 May 2026 10:57:51 |
| Eccentricity: | 0.0024396 |
| inclination: | 98.5481° |
| perigee height: | 677 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 139.2417° |
| argument of perigee: | 32.9707° |
| revolutions per day: | 14.59757594 |
| mean anomaly at epoch: | 327.3008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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