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 64529U 26145.60508795 +.00000000 +00000-0 +14981-3 0 00003
2 64529 97.4720 260.6168 0003531 242.5178 117.5699 15.20110339 00
| Epoch (UTC): | 25 May 2026 14:31:19 |
| Eccentricity: | 0.0003531 |
| inclination: | 97.4720° |
| perigee height: | 503 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 260.6168° |
| argument of perigee: | 242.5178° |
| revolutions per day: | 15.20110339 |
| mean anomaly at epoch: | 117.5699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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