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 27607U 26064.43584885 +.00000000 +00000-0 +31026-3 0 00003
2 27607 64.5518 89.9288 0075171 281.4760 77.7911 14.82762878 01
| Epoch (UTC): | 05 March 2026 10:27:37 |
| Eccentricity: | 0.0075171 |
| inclination: | 64.5518° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 89.9288° |
| argument of perigee: | 281.4760° |
| revolutions per day: | 14.82762878 |
| mean anomaly at epoch: | 77.7911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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