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 28538U 26156.69896954 +.00000000 +00000-0 +11067-3 0 00003
2 28538 63.8252 316.6153 0213395 255.7810 101.9432 13.43377786 09
| Epoch (UTC): | 05 June 2026 16:46:30 |
| Eccentricity: | 0.0213395 |
| inclination: | 63.8252° |
| perigee height: | 937 km |
| apogee height: | 1256 km |
| right ascension of ascending node: | 316.6153° |
| argument of perigee: | 255.7810° |
| revolutions per day: | 13.43377786 |
| mean anomaly at epoch: | 101.9432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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