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 52713U 26145.60450954 +.00000000 +00000-0 +82961-4 0 00002
2 52713 97.6272 94.8337 0001921 108.2398 251.9049 15.26009107 02
| Epoch (UTC): | 25 May 2026 14:30:29 |
| Eccentricity: | 0.0001921 |
| inclination: | 97.6272° |
| perigee height: | 486 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 94.8337° |
| argument of perigee: | 108.2398° |
| revolutions per day: | 15.26009107 |
| mean anomaly at epoch: | 251.9049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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