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 01587U 26162.26816723 +.00000000 +00000-0 +13785-3 0 00003
2 01587 56.0548 160.9868 0165438 302.0279 56.4642 12.38989795 07
| Epoch (UTC): | 11 June 2026 06:26:09 |
| Eccentricity: | 0.0165438 |
| inclination: | 56.0548° |
| perigee height: | 1380 km |
| apogee height: | 1641 km |
| right ascension of ascending node: | 160.9868° |
| argument of perigee: | 302.0279° |
| revolutions per day: | 12.38989795 |
| mean anomaly at epoch: | 56.4642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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