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 61953U 26145.39892506 +.00000000 +00000-0 +69079-3 0 00001
2 61953 53.1587 143.8098 0001395 90.6404 269.4762 15.42179871 00
| Epoch (UTC): | 25 May 2026 09:34:27 |
| Eccentricity: | 0.0001395 |
| inclination: | 53.1587° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.8098° |
| argument of perigee: | 90.6404° |
| revolutions per day: | 15.42179871 |
| mean anomaly at epoch: | 269.4762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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