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 65870U 26145.14595773 +.00000000 +00000-0 +42106-3 0 00004
2 65870 53.1601 298.8872 0001044 85.5036 274.6084 15.30206521 00
| Epoch (UTC): | 25 May 2026 03:30:10 |
| Eccentricity: | 0.0001044 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.8872° |
| argument of perigee: | 85.5036° |
| revolutions per day: | 15.30206521 |
| mean anomaly at epoch: | 274.6084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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