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 62875U 26145.25619157 +.00000000 +00000-0 +11812-2 0 00000
2 62875 53.1557 133.9103 0001050 95.0503 265.0618 15.30195488 06
| Epoch (UTC): | 25 May 2026 06:08:54 |
| Eccentricity: | 0.0001050 |
| inclination: | 53.1557° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.9103° |
| argument of perigee: | 95.0503° |
| revolutions per day: | 15.30195488 |
| mean anomaly at epoch: | 265.0618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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