▸Orbital parameters

Orbit class	SSO
Inclination	97.7746°
Eccentricity	0.0001621
Period	96.5 min
Apogee	593 km
Perigee	591 km
Mean motion	14.91883283 rev/day
RAAN	301.5115°
Arg of perigee	298.1220°
Mean anomaly	61.9835°
B*	2.0579e-4
Rev at epoch	5,680

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 64580U 25135BE 26187.93167830 .00002024 00000-0 20579-3 0 9994

2 64580 97.7746 301.5115 0001621 298.1220 61.9835 14.91883283 56803

▸ source OMM (JSON)

{
  "OBJECT_NAME": "YAM-10",
  "OBJECT_ID": "2025-135BE",
  "EPOCH": "2026-07-06T22:21:37.005+00:00",
  "MEAN_MOTION": 14.91883283,
  "ECCENTRICITY": 0.0001621,
  "INCLINATION": 97.7746,
  "RA_OF_ASC_NODE": 301.5115,
  "ARG_OF_PERICENTER": 298.122,
  "MEAN_ANOMALY": 61.9835,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64580,
  "REV_AT_EPOCH": 5680,
  "BSTAR": 0.00020579,
  "MEAN_MOTION_DOT": 0.00002024,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	YAM-10
Operator	Loft Orbital / EarthDaily AnalyticsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	150HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/64580

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.