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 45455U 26145.13135022 +.00000000 +00000-0 +70307-3 0 00001
2 45455 87.8908 25.6537 0002342 57.4931 302.6423 13.11414361 08
| Epoch (UTC): | 25 May 2026 03:09:08 |
| Eccentricity: | 0.0002342 |
| inclination: | 87.8908° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6537° |
| argument of perigee: | 57.4931° |
| revolutions per day: | 13.11414361 |
| mean anomaly at epoch: | 302.6423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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