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 53444U 26145.63996991 +.00000000 +00000-0 +70835-3 0 00009
2 53444 97.5515 274.6872 0003273 95.9093 264.2541 15.67806583 03
| Epoch (UTC): | 25 May 2026 15:21:33 |
| Eccentricity: | 0.0003273 |
| inclination: | 97.5515° |
| perigee height: | 363 km |
| apogee height: | 367 km |
| right ascension of ascending node: | 274.6872° |
| argument of perigee: | 95.9093° |
| revolutions per day: | 15.67806583 |
| mean anomaly at epoch: | 264.2541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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