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 52908U 26145.61867190 +.00000000 +00000-0 +91714-3 0 00008
2 52908 34.9953 207.8153 0004183 181.2880 178.7835 15.56651340 04
| Epoch (UTC): | 25 May 2026 14:50:53 |
| Eccentricity: | 0.0004183 |
| inclination: | 34.9953° |
| perigee height: | 395 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 207.8153° |
| argument of perigee: | 181.2880° |
| revolutions per day: | 15.56651340 |
| mean anomaly at epoch: | 178.7835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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