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 61887U 26145.25648594 +.00000000 +00000-0 +24379-4 0 00003
2 61887 53.1599 130.4905 0001077 90.4564 269.6562 15.34393627 08
| Epoch (UTC): | 25 May 2026 06:09:20 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.4905° |
| argument of perigee: | 90.4564° |
| revolutions per day: | 15.34393627 |
| mean anomaly at epoch: | 269.6562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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