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 48097U 26145.36453087 +.00000000 +00000-0 -24718-1 0 00009
2 48097 53.1608 156.3149 0016240 54.5856 305.6658 15.28529793 02
| Epoch (UTC): | 25 May 2026 08:44:55 |
| Eccentricity: | 0.0016240 |
| inclination: | 53.1608° |
| perigee height: | 469 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 156.3149° |
| argument of perigee: | 54.5856° |
| revolutions per day: | 15.28529793 |
| mean anomaly at epoch: | 305.6658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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