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 00045U 26129.92229096 +.00000000 +00000-0 +36722-4 0 00005
2 00045 66.6917 101.4082 0249728 188.8205 170.8471 14.35945359 02
| Epoch (UTC): | 09 May 2026 22:08:05 |
| Eccentricity: | 0.0249728 |
| inclination: | 66.6917° |
| perigee height: | 593 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 101.4082° |
| argument of perigee: | 188.8205° |
| revolutions per day: | 14.35945359 |
| mean anomaly at epoch: | 170.8471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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