▸Orbital parameters

Orbit class	SSO
Inclination	97.2326°
Eccentricity	0.0002354
Period	93.3 min
Apogee	436 km
Perigee	432 km
Mean motion	15.44090206 rev/day
RAAN	282.0961°
Arg of perigee	184.8514°
Mean anomaly	175.2712°
B*	9.4424e-6
Rev at epoch	10,608

▸Two-line element set (TLE)

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

1 60507U 24149AR 26187.91790435 .00000347 00000-0 94424-5 0 9992

2 60507 97.2326 282.0961 0002354 184.8514 175.2712 15.44090206106083

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TANAGER-1",
  "OBJECT_ID": "2024-149AR",
  "EPOCH": "2026-07-06T22:01:46.936+00:00",
  "MEAN_MOTION": 15.44090206,
  "ECCENTRICITY": 0.0002354,
  "INCLINATION": 97.2326,
  "RA_OF_ASC_NODE": 282.0961,
  "ARG_OF_PERICENTER": 184.8514,
  "MEAN_ANOMALY": 175.2712,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60507,
  "REV_AT_EPOCH": 10608,
  "BSTAR": 0.0000094424,
  "MEAN_MOTION_DOT": 0.00000347,
  "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	TANAGER-1
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia 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/60507

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