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 53473U 26145.66668980 +.00000000 +00000-0 +44732-2 0 00004
2 53473 97.5997 267.6150 0001266 73.0470 306.7379 15.25418983 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001266 |
| inclination: | 97.5997° |
| perigee height: | 489 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 267.6150° |
| argument of perigee: | 73.0470° |
| revolutions per day: | 15.25418983 |
| mean anomaly at epoch: | 306.7379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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