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 61702U 26145.35497542 +.00000000 +00000-0 -16282-3 0 00009
2 61702 53.1613 158.2392 0001476 87.9385 272.1787 15.34379306 00
| Epoch (UTC): | 25 May 2026 08:31:09 |
| Eccentricity: | 0.0001476 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.2392° |
| argument of perigee: | 87.9385° |
| revolutions per day: | 15.34379306 |
| mean anomaly at epoch: | 272.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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