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 53690U 26145.25029308 +.00000000 +00000-0 +25597-2 0 00003
2 53690 97.4465 25.1985 0001876 116.3590 243.7829 15.05459045 00
| Epoch (UTC): | 25 May 2026 06:00:25 |
| Eccentricity: | 0.0001876 |
| inclination: | 97.4465° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.1985° |
| argument of perigee: | 116.3590° |
| revolutions per day: | 15.05459045 |
| mean anomaly at epoch: | 243.7829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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